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In this lecture ...
• Solve problems related to– First law of thermodynamics for
closed and open systems– Heat engines– Refrigerators and heat pumps
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay2
Lect-13
Problem 1
• A 50 kg iron block at 80°C is dropped into an insulated tank that contains 0.5 m3 of liquid water at 25°C. Determine the temperature when thermal equilibrium is reached. Specific heat iron: 0.45 kJ/kgoC, specific heat of water: 4.184 kJ/kgoC
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay3
Lect-13
Solution: Problem 1
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay4
Lect-13
Ironm=50 kg
80oC
Water25oC
0.5 m3
Solution: Problem 1• Assumptions:
– Both water and the iron block are incompressible substances.
– Constant specific heats at room temperature can be used for water and the iron.
– The system is stationary and thus the kinetic and potential energy changes are zero, ΔKE, ΔPE=0 and ΔE= ΔU.
– There are no electrical, shaft, or other forms of work involved.
– The system is well-insulated and thus there is no heat transfer.
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay5
Lect-13
Solution: Problem 1• The energy balance can be expressed as:
ΔUsystem = ΔUiron + ΔUwater =0[mc(T2-T1)]iron + [mc(T2-T1)]water=0
Mass of water, m=V/v=0.5 m3/0.001 m3/kg= 500 kg
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay6
Lect-13
U
E-EE systemoutin
∆=
∆=
0
kJ)(
energies etc. potentialkinetic internal,in Change
mass and work heat,by nsferenergy traNet
Solution: Problem 1
• Substituting the above values,
(50kg)(0.45 kJ/kg oC)(T2 - 80oC) + (500 kg)(4.18 kJ/kg oC)(T2 - 25oC) =0
Therefore, T2 = 25.6oCThis will be the temperature of water and iron after the system attains thermal equilibrium.Note: The marginal change in the temperature of water. Why is this so?
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay7
Lect-13
Problem 2
• A stationary mass of gas is compressed without friction from an initial state of 0.3m3 and 0.105 MPa to a final state of 0.15 m3
and 0.105 MPa. There is a transfer of 37.6 kJ of heat from the gas during the process. What is the change in internal energy of the gas during this process?
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay8
Lect-13
Solution: Problem 2
• From the first law for a stationary system, Q=ΔU + W
• In this example, the process is a constant pressure process. The work done during such a process is
W=∫PdV=P(V2-V1)=0.105(0.15-0.30) = -15.75 kJ
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay9
Lect-13
Solution: Problem 2
• It is given that the heat transfer from the system is Q = -37.6 kJ
• Therefore, -37.6 = ΔU – 15.75or, ΔU = -21.85 kJ
• The change in internal energy of the gas is -21.85 kJ (decrease in internal energy during the process)
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay10
Lect-13
Problem 3
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay11
Lect-13
• Air at a temperature of 15oC passes through a heat exchanger at a velocity of 30 m/s where its temperature is raised to 800oC. It then passes through a turbine with the same velocity of 30 m/s and expands until the temperature falls to 650oC. On leaving the turbine, the air is taken at a velocity of 60 m/s to a nozzle where it expands until its temperature has fallen to 500oC. If the air flow rate is 2 kg/s, find (a) rate of heat transfer from the heat exchanger (b) the power output from the turbine (c) velocity at nozzle exit assuming no heat loss
• Assume cp= 1.005 kJ/kg K
Solution: Problem 3
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay12
Lect-13
1 2
3 4
Heat exchangerQ
WT
Turbine
Nozzle
T1=15oC, T2=800oCV1=30m/s, V2=30m/sT3=650oC, V3=60m/sT4=500oC
Solution: Problem 3
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay13
Lect-13
• Applying the energy equation across 1-2 (heat exchanger)
• The rate of heat exchanger to the air in the heat exchanger is 1580 kJ/s
kJ/s 1580)16.28816.1073(005.12
)()(
to,reduces thisexchanger,heat aFor
)(2
121221
12
21
22
12
=−××=
−=−=
−+
−+−=−
••
−
•
•••
TTcmhhmQ
zzgVVhhmWQ
p
Solution: Problem 3
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay14
Lect-13
• The energy equation the turbine 2-3
• The power output from the turbine is 298.8 kW
( ) ( )
kW8.2982
603016.92316.107310052
222
23
22
32
=
−+−××=
−+−=
•
••
W
VVhhmW
Solution: Problem 3
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay15
Lect-13
• For the nozzle (3-4)
• The velocity at the exit from the nozzle is 554 m/s.
smV
V
hVhV
/554
)16.773(005.12
)16.923(005.12
6022
4
24
2
4
24
3
23
=∴
×+=×+
+=+
Problem 4
• Heat is transferred to a heat engine from a heat source at a rate of 80 MW. If the rate of waste heat rejection to sink is 50 MW, determine the net power output and the thermal efficiency for this heat engine.
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay16
Lect-13
Solution: Problem 4
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay17
Lect-13
High temperature Source
Low temperature Sink
Heat Engine
QH=80 MW
QL=50 MW
Wnet,out
Solution: Problem 4
• We know that the net power output is the difference between the heat input and the heat rejected (cyclic device)
Wnet,out =QH + QL
= 80 – 50 MW= 30 MW • The net work output is 30 mW.• The thermal efficiency is the ratio of the
net work output and the heat input.ηth = Wnet,out/QH =30/80 = 0.375
• The thermal efficiency is 0.375 or 37.5 %
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay18
Lect-13
Problem 5
• The food compartment of a refrigerator is maintained at 4°C by removing heat from it at a rate of 360 kJ/min. If the required power input to the refrigerator is 2 kW, determine (a) the coefficient of performance of the refrigerator and (b) the rate of heat rejection to the room that houses the refrigerator.
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay19
Lect-13
Solution: Problem 5
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay20
Lect-13
Warm surroundings
Food compartment at 4oC
Refrigerator
QH
QL=360 kJ/min
Wnet,in=2 kW
Problem 5
• COP of the refrigerator, COPR=Desired effect/work input=QL/Wnet,in
=(360/60 kJ/s)/2 = 3 • The COP of the refrigerator is 3 (3 kJ of heat
is removed per kJ of work supplied).• The rate of heat rejection can be obtained
by applying the first law of thermodynamicsQH=QL+Wnet,in =6 kW + 2 KW = 8 kW
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay21
Lect-13
Problem 6
• A heat engine is used to drive a heat pump. The heat transfers from the heat engine and the heat pump are rejected to the same sink. The efficiency of the heat engine is 27% and the COP of the heat pump is 4. Determine the ratio of the total heat rejection rate to the heat transfer to the heat engine.
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay22
Lect-13
Solution: Problem 6
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay23
Lect-13
T1
T2
HeatPump
Q3
Q4
Heat Engine
Q1
W
T3
Q2
Solution: Problem 6
• The efficiency of the heat engine, ηη = Net work output/heat input = W/Q1
W = 0.27Q1
• COPHP = desired effect/work input= Q4/W = 4 or, W = Q4/4
• Therefore, 0.27Q1 = Q4/4 or, Q4/Q1= 1.08
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay24
Lect-13
Solution: Problem 6
• We know that η = 1-Q2/Q1 = 0.27Or, Q2/Q1 = 0.73
• Hence, (Q2+Q4)/Q1= 1.08 + 0.73 = 1.81• The ratio of the total heat rejection rate
(Q2+Q4) to the heat transfer to the heat engine (Q1) is 1.81.
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay25
Lect-13
Exercise Problem 1
• A mass of 8 kg gas expands within a flexible container as per pv1.2 = constant. The initial pressure is 1000 kPa and the initial volume is 1 m3. The final pressure is 5 kPa. If the specific internal energy of the gas decreases by 40 kJ/kg, find the heat transfer in magnitude and direction.
• Ans: +2615 kJ
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay26
Lect-13
Exercise Problem 2
• Air at 10°C and 80 kPa enters the diffuser of a jet engine steadily with a velocity of 200 m/s. The inlet area of the diffuser is 0.4 m2. The air leaves the diffuser with a velocity that is very small compared with the inlet velocity.
• Determine (a) the mass flow rate of the air and (b) the temperature of the air leaving the diffuser.
• Ans: 78.8 kg/s, 303K
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay27
Lect-13
Exercise Problem 3
• A refrigerator is maintained at a temperature of 2oC. Each time the door is opened, 420 kJ of heat is introduced inside the refrigerator, without changing the temperature of the refrigerator. The door is opened 20 times a day and the refrigerator operates at 15% of the ideal COP. The cost of work is Rs. 2.50 kWh. Determine the monthly bill for this refrigerator if the atmosphere is at 30oC.
• Ans: Rs. 118.80
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay28
Lect-13
Exercise Problem 4
• An automobile engine consumes fuel at a rate of 28 L/h and delivers 60 kW of power to the wheels. If the fuel has a heating value of 44,000 kJ/kg and a density of 0.8 g/cm3, determine the efficiency of this engine.
• Ans: 21.9%
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay29
Lect-13
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